N41CX, cancelled Jan 30, 2021
Service difficulty reports · 494
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N41CX' AND deregistration_id = 'N41CX-2021-01-30' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N41CX' AND deregistration_id = 'N41CX-2021-01-30' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IXXA201312040450Pressure Switch · malfunctionedAFTER TAKEOFF AT 1545Z NR 1 ENG LOW OIL PRESS LIGHT ILLUMINATED, PERFORMED APPROPRIATE CHECK LIST, LOW PRESS LIGHT STAYED ON SHUT ENG DOWN. R & R NR 1 LOW OIL PRESS SWITCH IAW 79-32-2, SYS OPERATIONS CHECKED NORMAL IAW DACO DC8 MM 79-32-0 & ATI ERH 70.01GMM 3SDR IXXA201308180280Bleed Valve · malfunctionedCOMPRESSOR STALL AT APPROX 75 KNOTS. SUSPECT NR 1 AND 2 ENGINES. RAN NR 1 AND 2 ENGINES IAW ENGINE RUN HANDBOOK 70.01. FOUND NR 1 ENGINE PRESSURE RATIO BLEED CONTROL VALVE WILL NOT CLOSE ABOVE 64 PERCENT N1. R & R PRESSURE RATIO BLEED CONTROL VALVE IAW MM 75SDR IXXA20130202002OLink · inoperativeON CLIMBOUT, AFTER A GOOD UPLATCH CHECK, HEARD A LOUD NOISE IN NOSE GEAR AREA. (SOUNDED LIKE A NOSE GEAR DOOR POPPED OPEN). R & R RT NLG DOOR FORWARD LINK ASSY IAW MM 32-22-1. OPS CHECKS GOOD ON NOSE GEAR SWING.SDR IXXA2013020700006Skin · crackedRT WING UPPER SKIN CRACKED AT XRS 22.750 S17. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIGURE 8. TRIMMED OUT CRACK ON RT WING UPPER SKIN IAW SRM 57-2-1. FABRICATED DOUBLER 0.190", FILLER 0.200" IAW SRM 57-2-1. CLEANED, TREATED AND PRIMED FABRICATED PARTS AND SDR IXXA2013020700005Panel · damagedRT WING OTBD FLAP LOWER PANEL WITH SEVERAL DENTS AND SCRATCHES XF 415 - 452. PERFORMED MAJOR REPAIR IAW SRM 57-7-1, FIG 4, TR 57-94. REMOVED OTBD FLAP LOWER PANEL IAW SRM 51-3-0. REMOVED EXISTING DAMAGED PANEL IAW SRM 51-1-21. FABRICATED NEW PANEL PLATING 0SDR IXXA2013020700004Fitting · corrodedAFTER CARGO COMPARTMENT - INTERIOR BATHTUB FITTING CORRODED AT STA 1530.000, L-32R (AFTER PART). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, NOV 15, 2012, DWG ED-5546 NOV 15, 2012. REMOVED CORRODED FITTING IAW SRM 51-1-20D, SRM 51-1-21. FABRICATED FITTING (SDR IXXA2013020700003Fitting · corrodedAFTER ACCESSORY COMPARTMENT INTERIOR BATHTUB FITTING CORRODED AT STA 1530.000 L-34R (AFTER PART). PERFORMED MAJOR REPAIR IAW FORM 8110-3 DWG NR ED-5546 NOV 15,2012. REMOVED CORRODED FITTING IAW SRM 51-1-20D, SRM 51-1-21. FABRICATED FITTING AL 7075T651 IAW DWSDR IXXA2013020700002Skin · corrodedRUDDER SKIN-LT PANEL SHOWS CORROSION FROM STA ZR 140.750 TO STA ZR 150.750. PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1. REMOVED EXISTING DAMAGED PANEL IAW SRM 51-1-21, SRM 55-1-0. FABRICATED NEW PANEL PLATING 0.016" AND BONDED DOUBLER 0.016" BOTH FROM AL 2SDR IXXA121109SMN026SLongeron · crackedLONGERON 24R, HORIZONTAL LEG CRACKED 2 INCHES AT FS 879.375. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 5 TR 53-123. REMOVED FASTENERS FROM REPAIRED AREA IAW SRM 51-1-20D.SDR IXXA121109SMN025SLongeron · crackedLONGERON 24L, HORIZONTAL LEG CRACKED 1 INCH AT FS 879.375. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 5, TR 53-123.SDR IXXA2013020700001Skin · damagedRT WING L/E NR 4 STUB WING CORRODED, XW 454 - XW 485. REMOVED FASTENERS FROM REPAIRED AREA IAW SRM 51-1-21. REMOVED CORROSION FROM DAMAGED AREA IAW SRM 51-1-8. TRIMMED OUT DAMAGED AREA IAW DWG ED-5545 NOV 14, 2012. FABRICATED DOUBLER 0.071" FILLER 0.063" BOSDR IXXA20120618016OConnector · dirtyNR 1 EGT FLUCTUATED RAPIDLY AND THEN DROPPED TO ZERO DURING TAKEOFF ROLL. TAKEOFF ABORTED AT APPROX 40 KNOTS. ACFT RETURNED TO BLOCKS. INSPECTED THERMOCOUPLE HARNESS JUNCTIONS. NO DEFECTS NOTED. REMOVED, CLEANED AND INSPECTED EGT HARNESS PYLON CONNECTOR. SDR IXXA20120605015Amplifier · failedCAPTAINS HSI AND ADI FAILED AFTER TAKEOFF. RETURNED TO ORIGINATING STATION. PERFORMED OVERWEIGHT LANDING INSP IAW MM 5-50-0 AND MM 13.01.05. NO DISCREPANCIES NOTED. R & R INSTRUMENT AMPLIFIER IAW MM 34-23-00. OPS CHECKED GOOD.SDR IXXA20120605014Gyro · failedCAPTAINS HSI AND ADI FAILED AFTER INITIAL CLIMBOUT AND LEVEL OFF AT CRUISE ALTITUDE. RETURNED TO ORIGINATING STATION. R & R NR 1 FOG GYRO IAW MM 34-11-25. OPS CHECKED GOOD.SDR IXXA20120228005OSwitch · leakingNR 3 ENGINE STARTED SLOWLY LEAKING OIL. AT 1418Z WITH NR 3 OIL QUANTITY INDICATION OF 1 GALLON AND NR 3 OIL TEMP SLOWLY STARTING TO INCREASE, NR 3 ENGINE WAS SHUTDOWN AS A PRECAUTION. AFTER SHUTDOWN, NR 3 ENGINE OIL QUANTITY CONTINUED TO DECREASE TO ZERO WITH SDR IXXA20120218003OBattery · inoperativeDURING PREFLIGHT INSPECTION, FOUND RT EMERGENCY FLASHLIGHT INOPERATIVE. MX REPLACED EMERGENCY FLASHLIGHT BATTERY. OPS CHECKED GOOD IAW MM 25-60-0.SDR IXXA1100740Fan · failedDURING DESCENT, FLIGHT CREW SWITCHED ON RT RECIRCULATION FAN AND NOTICED A STRONG ELECTRICAL ODOR. FAN WAS SUBSEQUENTLY TURNED OFF AND ELECTRICAL ODOR DISSIPATED. MX TROUBLESHOT AND R & R RT RECIRCULATION FAN IAW MM 21-21-1.SDR IXXA110069OTransceiver · defectiveDURING CLIMB OUT, THE WEATHER RADAR FAILED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED WEATHER RADAR TRANSCEIVER, OPS CHECK GOOD IAW MM 34-40-02. ACFT WAS RETURNED TO SERVICE.SDR IXXA20110813001Skin · corrodedDURING ROUTINE C-CHECK INSP, FOUND VERTICAL STABILIZER RT LATERAL SKIN CORRODED AT STA ZR 35.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IASDR IXXA20110812001Spar · corrodedDURING ROUTINE C-CHECK INSP FOUND RT VERTICAL STABILIZER REAR SPAR CORRODED AT STA ZR 45.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED STRAP AND FILLER. CLEANED, TREATED, PRIMED AREA SDR IXXA20110811001Skin · corrodedDURING ROUTINE C-CHECK INSP, FOUND LT WING T/E UPPER SKIN CORRODED AT STA XW 761.695 - 736.500. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED REPAIR PARTS AS NEEDED. CLEANED, TREATED, PRIMED ARESDR IXXA20110810003Skin · crackedDURING ROUTINE C-CHECK INSP, FOUND RT INBD AILERON UPPER SKIN CRACKED AT STATION XA 603.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. PERFORMED RT INBD AILERON BSDR IXXA20110810002Skin · crackedDURING ROUTINE C-CHECK INSP, FOUND RT OTBD AILERON LOWER SKIN CRACKED AT STA XA 610.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. PERFORMED RT OTBD AILERON BALASDR IXXA20110810001Angle · crackedDURING ROUTINE C-CHECK, INSP FOUND NR 60 ACCESS DOOR BEAM AFT PRESS BULKHEAD CRACKED BOTTOM LINE-0. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP HOLE AT CRACK END. FABRICATED ANGLES FORMED AND PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRISDR IXXA11SMN103SSkin · corrodedDURING ROUTINE C-CHECK, FOUND EXTERNAL SKIN CORRODED AT BS 902.00- 910.000 LONGERON 19 - 21RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCIES FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER AND FILLERSDR IXXA20110809004Skin · corrodedDURING ROUTINE C-CHECK INSP FOUND EXTERNAL SKIN CORRODED AT STA 1100.000 LONGERON 21 RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER AND FILLER. CLEANED, TREATED, SDR IXXA20110809003Skin · corrodedDURING ROUTINE C-CHECK INSP FOUND LT WING UPPER SKIN CORRODED AT STATION XRS 358.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER AND MACHINE TAPERED DOUBLER. CLEASDR IXXA20110809001Skin · corrodedDURING ROUTINE C-CHECK INSP FOUND LT WING UPPER SKIN AFT PART CORRODED AT STA XRS 70.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER AND MACHINE TAPERED DOUBLSDR IXXA20110808002Skin · corrodedDURING ROUTINE C-CHECK INSP FOUND FORWARD CARGO COMPARTMENT INTERNAL SKIN CORRODED AT STA 600.000, LONGERON 36. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLERSDR IXXA20110808001ASkin · crackedDURING ROUTINE C-CHECK INSP FOUND FUSELAGE NOSE SECTION LOWER SKIN CRACKED AT STA 260.000, LONGERON 34 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER AND FSDR IXXA20110808001Skin · crackedDURING ROUTINE C-CHECK INSP, FOUND NLG CORNER LOWER SKIN CRACKED AT STATION 208.000, LONGERON 33 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER AND FILLER. CLEANED, SDR IXXA20110801002Structure · misrepairedDURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR AT STA FS 255 LONGERON 33.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER, FILLER, AND FINGER DOUBLERS. CLEANEDSDR IXXA201108SMN095SAngle · crackedDURING ROUTINE C-CHECK INSP, FOUND ANGLE CRACKED AT STA FS 975 LONGERON 24 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR ANGLE. CLEANED, TREATED, PRIMED AREA AND REPAIR. INSTALLED NEW FASTENERS AND REPAIR ANGLE IASDR IXXA100059OCoupler · defectiveDURING CRUISE, NR1 HF RADIO WILL NOT CHANNELIZE AND HAD NO RECEPTION, NR 2 HF RADIO WOULD NOT WORK. THE CREW RETURNED TO DEPARTURE WITH OUT FURTHER INCIDENT. MX REPLACED NR1 ACCESSORY COUPLER AND 2 COAX CONNECTORS ON THE NR2 ACCESSORY COUPLER. OPS CHECK GOOD SDR IXXA100054ODuct · disconnectedDURING CRUISE, NR 4 ENGINE GENERATOR UNPARALLEL LIGHT FOLLOWED BY GENERATOR DRIVE OIL LIGHT, MANIFOLD PRESSURE LIGHT ILLUMINATED WITH HIGH PRESSURE MANIFOLD AIR PRESSURE OVERTEMP LIGHT CAME ON, LOSS OF EGT INDICATION, ZERO FUEL FLOW AND ZERO EPR. THE CREW SHUTSDR IXXA100052SSkin · crackedDURING INSP, FOUND SKIN CRACKED AT STA 255 BETWEEN LONGERONS 33 AND 34 RT SIDE. INSTALLED INTERIM REPAIR IAW REA D853-60270.SDR IXXA090077OO-Ring · damagedDURING CRUISE, ACFT LOST HYD FLUID TO THE STANDPIPE LEVEL. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MX INSPECTED THE HYD SYS AND FOUND THE O-RING ON THE NR 2 SYS HYD PUMP PRESSURE LINE LEAKING. THE O-RING WAS REPLACED, THE LEAK AND OPS CHECKS WERE GOOD ANSDR IXXA090072OEngine · power lossDURING TAKEOFF FROM WSAP NR 4 ENG FAILED TO PRODUCE TAKEOFF PWR. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX PERFORMED POWER RUN AND ACCELERATION CHECK. OPS CHECK GOOD IAW ERH 72.01.1. ACFT WAS RETURNED TO SERVICE.SDR IXXA090068OPrbc · dryDURING CLIMB OUT, THE CREW HEARD A LOUD BANG, F/A REPORTED A FLASH ON LT SIDE. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED BOTH NR 1 AND NR 2 ENGINE'S, LUBED THE PRBC'S. OPS CHECK GOOD IAW MM 72-00, ERH 70.01, ERH 75.01, AND MM 12-80-0. SDR IXXA090063OReservoir · lowDURING CLIMB OUT FROM RJTY THE CREW NOTICE HYDRAULIC FLUID DROPPED TO STANDPIPE WITH RESERVOIR LOW PRESSURE LIGHT ON, THE CREW RETURNED TO RJTY WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED HYDRAULIC RESERVOIR. OPERATIONAL CHECK GOOD IAW MM 12-30-1, ERH 70.01SDR IXXA090055OFan · defectiveDURING C CHECK TEST FLIGHT FROM SPLP THE LEFT HAND RECIRCULATION FAN EMITTED ELECTRICAL ODOR. THE CREW TURNED OFF LEFT RECIRCULATION FAN. THEY RETURNED TO SPLP WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT HAND RECIRCULATION FAN. OPERATIONAL CHECK SDR IXXA09SMN094SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND FUSELAGE EXTERNAL SKIN CORRODED AT STA 960.000 LONGERON 18-19 RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASETNERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. PERFORMED NDT INSP. NO CRACK OR COSDR IXXA09SMN093SSkin · dentedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING INBOARD AILERON UPPER SKIN DENTED AT STATION XA 515.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED,SDR IXXA09SMN092SSkin · crackedDURING ROUTINE C CHECK INSPECTION FOUND LT WING INBOARD AILERON UPPER SKIN CRACKED AT STATION XW 563.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, SDR IXXA09SMN091SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RUDDER LT SKIN CORRODED AT STATION ZR 238.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, AND PRIMED AREA SDR IXXA09SMN090SFitting · crackedDURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT SUB FLOOR FITTING CRACKED AT STATION 798.000 LBL 24". REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-0, DC8 SRM 51-1-8BSDR IXXA09SMN089SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND RT WING L/E LWR SKIN CORRODED AT STA XFS 566.250. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK OR CORROSION. FABRICATED DOUBLER, AND FILLER. CLEANED, TREATED, AND PRIMED AREA ANSDR IXXA09SMN087SSpar Cap · corrodedDURING ROUTINE C-CHECK INSP, FOUND RUDDER RT SIDE FRONT SPAR CAP CORRODED AT STA ZR 323.000. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED DAMAGED SPAR CAP. FABRICATED NEW SPAR CAP. CLEANED, TREATED, AND PRIMED AREA AND NEW SPAR CAP. INSTALLED NEW SPAR CAP SDR IXXA09SMN088SLongeron · corrodedDURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT CORROSION ON LONGERON 22 RT AT STATION 1530.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED LONGERON. CLEANED, TREATED, AND PRIMED AREA AND LONGERON. INSTALLED NEW LONGERON IAW SRM CHASDR IXXA09SMN086SAngle · corrodedDURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT AFT RING ANGLE CORRODED AT STATION 1530.000 LONGERON 26-28 LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR ANGLE. FABRICATED REPAIR ANGLE SPLICE. CLEANED, TREATED, AND PRIMED AR
Back to N41CX, cancelled Jan 30, 2021